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The effect of \(C_{22}\) on orbit energy and angular momentum

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Publication:1976109
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DOI10.1023/A:1008384021964zbMath0971.70016OpenAlexW4247116908MaRDI QIDQ1976109

Daniel J. Scheeres

Publication date: 1 November 2001

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1008384021964


zbMATH Keywords

angular momentumJacobi integralPicard's methodescapeCastaliahyperbolic orbitnumerical integrationscanonical elementsparabolic orbitbody-fixed coordinate systemErosC(22) gravity termfirst iterationhigh eccentric elliptic orbitIdaisolated uniform rotating bodyorbit energy


Mathematics Subject Classification ID

Two-body problems (70F05) Celestial mechanics (70F15)


Related Items (5)

A method for classifying orbits near asteroids ⋮ Closed-form normalizations of perturbed two-body problems. ⋮ Nonlinear stability of the equilibria in a double-bar rotating system ⋮ Science orbit design with a quasi-frozen beta angle: effects of body obliquity on J2-perturbed dynamics ⋮ Approximating orbits in a rotating gravity field with oblateness and ellipticity perturbations







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